Aluminium 5052

Aluminium alloy, primarily alloyed with 2.5% magnesium and 0.25% chromium. This is one of the highest strength non-age hardenenable alloys available.


Uses
Aircraft wing ribs, fuel tanks and framework.

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Tensile strength 90000000 Nm-2Clip
Yield strength 195000000 Nm-2Clip
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Subjects: Chemistry